Effects of bondline flaws on the damage tolerance of composite scarf joints

Author:

Goh J.Y.,Georgiadis S.,Orifici A.C.,Wang C.H.

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference45 articles.

1. A proposed approach for certification of bonded composite repairs to flight-critical airframe structure;Baker;Appl Compos Mater,2011

2. FAA. FAA Federal Aviation Regulations (FAR) Part 23. Section 573-Damage tolerance and fatigue evaluation of structure; 2005.

3. FAA. Composite aircraft structure: advisory circular (AC) 20-107B, Change 1, FAA; 2010.

4. Residual strength of composite laminates containing scarfed and straight-sided holes;Wang;Compos A: Appl Sci Manuf,2011

5. Harman AB, Wang CH. Damage tolerance and impact resistance of composite scarf joints. Proceedings of 16th International Conference on Composite Materials, Kyoto, Japan.http://www.iccm-central.org/Proceedings/ICCM16proceedings/contents/pdf/TueH/TuHM1-06ge_harmana220504p.pdf

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